View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68530U 26145.24668325 +.00000000 +00000-0 +63160-3 0 00008
2 68530 53.1585 133.8465 0001083 84.9635 275.1490 15.30201395 05
| Epoch (UTC): | 25 May 2026 05:55:13 |
| Eccentricity: | 0.0001083 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.8465° |
| argument of perigee: | 84.9635° |
| revolutions per day: | 15.30201395 |
| mean anomaly at epoch: | 275.1490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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